EFIS-D6 Installation Guide

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Appendix these lines, you may drill all the way through the outer metal without affecting the probe’s waterproofing. DIMENSIONS Standard mount 5-12 EFIS-D6 Installation Guide
Appendix Boom mount PLUMBING NOTE: Because the pitot and AOA plumbing tubes have not been annealed, they work-harden rapidly when manipulated. Make gentle bends, and only bend any given section once. After mounting the probe, route the pitot and AOA lines from the probe to your EFIS-D6. The tube closest to the snout is the pitot line, while the tube in the rear is the AOA line. There is no static source on the probe. After mounting the probe, install adapters to connect the 3/16 plumbing lines from the probe to whatever plumbing lines run back to the EFIS-D6 in your aircraft (AN 919-2D for 3/16 to ¼). We strongly recommend using aircraft grade fittings such as standard AN fittings. Make sure the plumbing lines do not chafe or interfere with any aircraft control systems. PRESSURE CHECK Dynon’s pitot design deliberately has a pin-sized leak hole in each of the two tubes to permit draining any moisture which might accumulate inside. These holes are located in the middle of the tube at the bottom. Plugging these holes does not guarantee a pneumatic seal (although one is sometimes present). The leak that may exist does not affect the performance of the probe. You will, however, need to take it into account when doing pressure/leak tests on your pitot system CALIBRATION CAUTION: It is your responsibility to fly your plane safely while performing any configuration or calibration in flight. The best scenario would include a second person to perform any necessary steps on the EFIS-D6. Once you are flying straight and level at a safe altitude for stalls, enter the EFIS > SETUP > AOACAL menu. While the AOACAL menu is displayed, oscillate the aircraft between ± 5° pitch 4 times at fast cruise airspeed. During this maneuver the EFIS-D6 records the lowest angle of attack that you usually see during flight. You do not need to push any additional buttons before starting this maneuver. Refer to the list below of the stalls recommended to complete the user calibration. The general idea is to record stall data to find the lowest angle of attack stall. The list we have suggested is a starting point and produces a good calibration under most circumstances. However, if there are EFIS-D6 Installation Guide 5-13
Page 1: EFIS-D6 Installation Guide This pro
Page 5: Table of Contents Contact Informati
Page 8 and 9: Introduction About this Guide In th
Page 10 and 11: Wiring Overview 25-Pin Female EFIS
Page 12 and 13: Wiring Overview WIRING SYSTEM OVERV
Page 14 and 15: Instrument Installation D10A is ali
Page 16 and 17: Instrument Installation PC CONNECTI
Page 18 and 19: Instrument Installation SERIAL ALTI
Page 20 and 21: Instrument Installation Panel Locat
Page 22 and 23: Instrument Installation Connecting
Page 24 and 25: EFIS Calibration and Configuration
Page 31 and 32: 5. APPENDIX The appendices contain
Page 33 and 34: Alert Message Description End condi
Page 35 and 36: Appendix Problem Airspeed is inaccu
Page 37 and 38: Appendix Appendix B: Dynon AOA/Pito
Page 39 and 40: Appendix instructions on the follow
Page 41: Appendix controller. Remember that
Page 45 and 46: Appendix Appendix C: Encoder Serial
Page 47 and 48: Appendix EFIS DB25 Pin# 13 Dynon EF
Page 49 and 50: Appendix Appendix E: Upgrading EFIS

EFIS-D6 Installation Guide

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